JPH0637597U - Stationary blade angle changing device - Google Patents
Stationary blade angle changing deviceInfo
- Publication number
- JPH0637597U JPH0637597U JP7884192U JP7884192U JPH0637597U JP H0637597 U JPH0637597 U JP H0637597U JP 7884192 U JP7884192 U JP 7884192U JP 7884192 U JP7884192 U JP 7884192U JP H0637597 U JPH0637597 U JP H0637597U
- Authority
- JP
- Japan
- Prior art keywords
- lever
- pin
- groove
- stationary blade
- hole
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Withdrawn
Links
Abstract
(57)【要約】
【目的】 静翼々角変更装置において、車室に正確に半
径方向に開ける穴の数を半減し、加工コストの低減を図
る。
【構成】 レバーを第1のレバー2、第2のレバー4の
如く2重に設け、第2のレバー4は一端を静翼軸1に回
転自由に嵌め込み、他端にピン5を設け、同ピン5を円
環の溝に係合させ、中間位置にピン6を設ける。一方第
1のレバー2は静翼軸1にピン3により固定し、他端に
ピン6に係合する溝2aを設けてなるものである。
(57) [Abstract] [Purpose] In the stator vane angle changing device, the number of holes to be accurately made in the radial direction in the vehicle compartment is halved to reduce the machining cost. [Structure] A lever is provided in a double manner like a first lever 2 and a second lever 4, one end of the second lever 4 is rotatably fitted to a stationary blade shaft 1, and a pin 5 is provided at the other end. The pin 5 is engaged with the groove of the ring, and the pin 6 is provided at the intermediate position. On the other hand, the first lever 2 is fixed to the stationary blade shaft 1 by a pin 3 and is provided with a groove 2a for engaging with the pin 6 at the other end.
Description
【0001】[0001]
本考案は軸流圧縮機の静翼々角変更装置に関するものである。 The present invention relates to a stator vane angle changing device for an axial compressor.
【0002】[0002]
軸流圧縮機では性能上、或いは運転許容範囲を拡げる目的で静翼取付角を運転 中に任意に変更する事がしばしば行なわれる。その場合の一般的な方法は次の如 くである。即ち、前方の複数段を可変とする(段数は具体的な設計により変わる 。図4に示した例では入口案内弁(1GV)、第1段静翼(1C)、第2段静翼 (2C)、第3段静翼(3C)の前方4段)。また動かす角度は前方から後方に 向かい順次小とする。更に云えば前方からの段数に反比例させる事が多く、具体 的な数値で示せば、前方から1段を10°動かすとすると、第2段目は7.5° 、第3段目は5°、第4段目は2.5°である(第5段目以降は固定)。なお、 図中1は静翼軸、8は車室、14は操作環である。 また1個の円環でこの関係を実現しようとすると、静翼のレバーの長さは後方 に行くに従って長くしなければならず、前記の例で云えば第4段目は、第1段目 のレバーに対し約4倍の長さを要する(取付角が傾斜するとその影響が入るので 正確に4ではなくなる)。 この様な例を図5に示す。また動かすべき段数が増すと、例えば5段とすると 5段目のレバー長さは第1段目の5倍にならなければならないが、これは実際の 設計では図5から推測される様に甚だ難しい問題であった。この困難さを解決す る為に、従来も図6及び図7に示す如き2重レバーとする考えが提案された。 In axial flow compressors, the vane mounting angle is often changed arbitrarily during operation for the purpose of expanding performance or operating allowable range. The general method in that case is as follows. That is, the front multiple stages are made variable (the number of stages varies depending on the specific design. In the example shown in FIG. 4, the inlet guide valve (1 GV), the first stage vane (1C), the second stage vane (2C), the third stage Stepped vanes (4 steps forward of 3C). In addition, the angle of movement will be smaller from front to back. In addition, it is often inversely proportional to the number of steps from the front, and in concrete terms, if one step is moved 10 ° from the front, the second step is 7.5 ° and the third step is 5 °. , The fourth stage is 2.5 ° (fixed after the fifth stage). In the figure, 1 is a stationary blade shaft, 8 is a vehicle interior, and 14 is an operation ring. In order to realize this relationship with one ring, the length of the lever of the stationary blade must be made longer toward the rear. In the above example, the fourth stage is the first stage. Approximately 4 times as long as the lever of (It will not be exactly 4 because the effect will occur if the mounting angle is tilted). Such an example is shown in FIG. Also, if the number of steps to be moved increases, for example, if the number of steps is 5, the lever length at the 5th step must be 5 times as long as at the 1st step, but this is serious in actual design as can be inferred from Fig. 5. It was a difficult problem. In order to solve this difficulty, the idea of using a double lever as shown in FIGS. 6 and 7 has been proposed in the past.
【0003】[0003]
しかしながら前記従来の図6及び図7の例では次のような問題があった。即ち 、2重レバーを設ける段にあっては、車室に翼を取付ける穴とは別に第2のレバ ーを取付ける穴を設けなければならなかった。 しかもこの穴は翼を取付ける穴と全く同じ正確さで加工しなければならず、言 い換えると正確な寸法の穴を2倍加工する事に近かった。また大きな円環の外周 に、半径方向に正確なピッチで正確な寸法の穴を多数加工する事は、コスト上甚 だ不利であった。 本考案は前記従来の問題を解決しようとするものである。 However, the conventional examples of FIGS. 6 and 7 have the following problems. That is, at the stage where the double lever was provided, a hole for mounting the second lever had to be provided separately from the hole for mounting the wing in the passenger compartment. Moreover, this hole had to be machined with exactly the same accuracy as the hole to install the blade, in other words, it was close to double the hole of the correct size. In addition, it was very disadvantageous in terms of cost to machine a large number of holes on the outer circumference of a large ring with an accurate pitch in the radial direction. The present invention is intended to solve the above conventional problems.
【0004】[0004]
このため本考案は、流体機械の静翼々角を任意に運転中に変更する装置であっ て、静翼の一端に軸を設けると共に、同軸端にレバーを設け、同レバーの他端に ピンを設け、かつ車室の外側に円周溝を設けた円環を設け、同円周溝にレバーの ピンを係合させて円環を軸方向に動かす事により、或いはレバーの他端に溝又は 穴を設け、車室外周に設けた円環に植込んだピンを同穴又は溝に係合させて円環 を周方向又は軸方向に移動させる事により、静翼々角を一斉に動かす静翼々角変 更装置において、レバーを2重に設け、一方のレバーは一端を静翼軸に回転自由 に嵌め込み、他端を円環の溝又はピンに係合させると共に、中間位置にピン、溝 又は穴を設け、他方のレバーは前記静翼軸に固定し、他端を前述のレバーの前記 中間位置のピン、溝又は穴に係合する穴、溝又はピンを設けてなるもので、これ を課題解決のための手段とするものである。 Therefore, the present invention is a device for arbitrarily changing the vane angles of a fluid machine during operation.A shaft is provided at one end of the vane, a lever is provided at the coaxial end, and a pin is provided at the other end of the lever. By providing a circular ring with a circular groove on the outside of the passenger compartment and engaging the pin of the lever with the circular groove to move the circular ring in the axial direction, or at the other end of the lever. By providing a hole and engaging a pin implanted in an annular ring provided on the outer periphery of the vehicle compartment with the hole or groove to move the annular ring in the circumferential or axial direction, the stationary vanes that move the stationary vanes all at once In the angle changing device, two levers are provided, one lever is rotatably fitted to the stator shaft at one end, and the other end is engaged with the groove or pin of the ring, and the pin, groove or A hole is provided, the other lever is fixed to the vane shaft, and the other end is a pin at the intermediate position of the lever. Holes engaging the groove or hole, those formed by providing a groove or a pin, it is an unit for which a problem solution.
【0005】[0005]
静翼軸は第2のレバーの動きを第1のレバーによりX/Y倍縮小されて動く。 即ち、第2のレバーで直接静翼軸を動かす場合には、円環の軸方向の動き単位量 に対し、≒1/Z radの角度動く。それに対して第1のレバーを組合せる事 により≒X/ZY radの角度変化となる。なお、Xの長さは静翼軸の直径の 兼合いから無暗に小とする事は出来ないので、縮小の割合は実際の設計では自ず と制限はあるものの、単一レバーに対し動かす角度を充分小さく出来る。また従 来方式に比べてピン穴を省略出来る。即ち、本考案を適用する段に関しては、加 工費用の嵩む穴を半減出来る。 The stationary blade axis is moved by reducing the movement of the second lever by X / Y times by the first lever. That is, when the stationary blade shaft is directly moved by the second lever, an angle of ≉1 / Z rad is moved with respect to the unit movement amount of the annular ring in the axial direction. On the other hand, by combining the first lever, an angle change of ≈X / ZY rad results. It should be noted that the length of X cannot be reduced indiscriminately due to the trade-off of the diameter of the stationary blade axis, so although the reduction rate is naturally limited in the actual design, it can be moved with respect to a single lever. The angle can be made small enough. Also, the pin hole can be omitted as compared with the conventional method. That is, with respect to the stage to which the present invention is applied, the hole costly for processing can be reduced by half.
【0006】[0006]
【実施例】 以下本考案を図面の実施例について説明すると、図1〜図3は本考案の実施例 を示す。先ず本考案の第1実施例を示す図1〜図2について説明すると、1は静 翼軸、2は第1のレバー、3はピン、4は第2のレバー、5はピン、6もピン、 7は第2のレバー4を操作する方向を示す。 さて図1及び図2において、静翼の一端の車室8に支持された静翼軸1の軸端 に、第1のレバー2と第2のレバー4を上下に組合せて設けると共に、レバー4 の他端にピン5を設け、一方車室8の外側に円周溝を設けた円環を設け、同円周 溝にレバー4のピン5を係合させて同円環を軸方向に動かすことにより、静翼々 角を一斉に動かすようにしたものである。即ち、レバーを第1のレバー2、第2 のレバー4の如く2重に設け、第2のレバー4は一端を静翼軸1に回転自由に嵌 め込み、他端にピン5を設け、同ピン5を円環の溝に係合させ、中間位置にピン 6を設ける。一方第1のレバー2は静翼軸1にピン3により固定し、他端にピン 6に係合する溝2aを設けてなるものである。なお、第2のレバー4に設けた前 記ピン6に代えて溝又は穴を設け、前記第1のレバー2の溝2aに代えてピンを 設けても差し支えない。DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS The present invention will be described below with reference to the embodiments of the drawings. FIGS. 1 to 3 show the embodiments of the present invention. 1 to 2 showing the first embodiment of the present invention, 1 is a stationary blade shaft, 2 is a first lever, 3 is a pin, 4 is a second lever, 5 is a pin, and 6 is also a pin. , 7 indicates the direction in which the second lever 4 is operated. 1 and 2, the first lever 2 and the second lever 4 are vertically combined at the shaft end of the vane shaft 1 supported by the casing 8 at one end of the vane, and the lever 4 is combined. Is provided with a pin 5 at the other end thereof, and on the other hand, an annular ring having a circumferential groove is provided outside the vehicle compartment 8, and the pin 5 of the lever 4 is engaged with the circumferential groove to move the annular ring in the axial direction. As a result, the stationary vanes are moved all at once. That is, the lever is provided in double like the first lever 2 and the second lever 4, one end of the second lever 4 is rotatably fitted to the stationary blade shaft 1, and the pin 5 is provided at the other end. The pin 5 is engaged with the groove of the ring, and the pin 6 is provided at the intermediate position. On the other hand, the first lever 2 is fixed to the stationary blade shaft 1 by a pin 3 and is provided with a groove 2a at the other end for engaging with the pin 6. A groove or a hole may be provided in place of the pin 6 provided on the second lever 4, and a pin may be provided instead of the groove 2a of the first lever 2.
【0007】 なお、図1及び図2では第2のレバー4に第1のレバー2を動かすピン6を植 込んだ状態を示しているが、逆の組合せも可能である。即ち、第1のレバー2と 第2のレバー4を上下逆に組合せる事も可能である。 図1及び図2では、円環を軸方向に動かす場合を示しているが、図3には円環 を周方向に動かす場合の構造の図2に対応するものを示している。図3において 10は第1のレバー、11は第2のレバー、12は第2のレバー11で第1のレ バー10を動かすピン、13は第2のレバー11を操作する方向を示す。Although FIGS. 1 and 2 show the state in which the pin 6 for moving the first lever 2 is implanted in the second lever 4, the reverse combination is also possible. That is, it is possible to combine the first lever 2 and the second lever 4 upside down. 1 and 2 show a case where the ring is moved in the axial direction, FIG. 3 shows a structure corresponding to FIG. 2 when the ring is moved in the circumferential direction. In FIG. 3, 10 is a first lever, 11 is a second lever, 12 is a pin for moving the first lever 10 with the second lever 11, and 13 is a direction for operating the second lever 11.
【0008】[0008]
以上詳細に説明した如く本考案によれば、半径方向に正確に開けなければなら ない穴を半減出来る。従来の如く大きな車室に半径方向に正確な角度とピッチで 、正確な直径の穴を多数開ける事はコストが嵩むが、本考案ではこの穴を半減出 来るためコスト上有利である。またレバーの形状が従来と多少変わっても、加工 する穴数、ピンの数などの面で本考案の場合が逆に特に不利になるようなことは 無い。 As described in detail above, according to the present invention, the number of holes that must be accurately drilled in the radial direction can be reduced by half. Although it is costly to form a large number of holes having an accurate diameter and an accurate pitch in the radial direction in a large passenger compartment as in the conventional case, the present invention is advantageous in cost because the holes are halved. Further, even if the shape of the lever is slightly different from the conventional one, there is no particular disadvantage in the case of the present invention in terms of the number of holes to be machined and the number of pins.
【図1】本考案の第1実施例に係る静翼々角変更装置の
断面図である。FIG. 1 is a sectional view of a stator vane angle changing device according to a first embodiment of the present invention.
【図2】図1の平面図である。FIG. 2 is a plan view of FIG.
【図3】本考案の第2実施例に係る静翼々角変更装置の
平面図である。FIG. 3 is a plan view of a stator vane angle changing device according to a second embodiment of the present invention.
【図4】従来の圧縮機における静翼部分の断面図であ
る。FIG. 4 is a cross-sectional view of a vane portion of a conventional compressor.
【図5】図4のA〜A断面図である。5 is a sectional view taken along line AA of FIG.
【図6】従来の図4と異なる圧縮機の静翼部分を示す断
面図である。FIG. 6 is a cross-sectional view showing a stationary blade portion of a compressor different from the conventional compressor shown in FIG.
【図7】図6のB矢視図である。FIG. 7 is a view on arrow B of FIG.
1 静翼軸 2 第1のレバー 2a 溝 3 ピン 4 第2のレバー 5 ピン 6 ピン 7 第2のレバーを操作する方向 1 stationary blade shaft 2 first lever 2a groove 3 pin 4 second lever 5 pin 6 pin 7 direction to operate second lever
───────────────────────────────────────────────────── フロントページの続き (72)考案者 藤岡 渡 兵庫県高砂市荒井町新浜二丁目8番25号 高菱エンジニアリング株式会社内 ─────────────────────────────────────────────────── ─── Continuation of the front page (72) Inventor Wataru Fujioka 2-8-25, Niihama, Arai-cho, Takasago-shi, Hyogo Takahishi Engineering Co., Ltd.
Claims (1)
更する装置であって、静翼の一端に軸を設けると共に、
同軸端にレバーを設け、同レバーの他端にピンを設け、
かつ車室の外側に円周溝を設けた円環を設け、同円周溝
にレバーのピンを係合させて円環を軸方向に動かす事に
より、或いはレバーの他端に溝又は穴を設け、車室外周
に設けた円環に植込んだピンを同穴又は溝に係合させて
円環を周方向又は軸方向に移動させる事により、静翼々
角を一斉に動かす静翼々角変更装置において、レバーを
2重に設け、一方のレバーは一端を静翼軸に回転自由に
嵌め込み、他端を円環の溝又はピンに係合させると共
に、中間位置にピン、溝又は穴を設け、他方のレバーは
前記静翼軸に固定し、他端を前述のレバーの前記中間位
置のピン、溝又は穴に係合する穴、溝又はピンを設けた
ことを特徴とする静翼々角変更装置。1. A device for arbitrarily changing the vane angles of a fluid machine during operation, wherein a shaft is provided at one end of the vane,
A lever is provided at the coaxial end, and a pin is provided at the other end of the lever,
A ring with a groove is provided outside the passenger compartment, and the pin of the lever is engaged with the groove to move the ring in the axial direction, or a groove or hole is formed at the other end of the lever. Change the stationary blade angle by moving the stationary blade angle all at once by engaging the pin embedded in the annular ring provided on the outer periphery of the vehicle compartment with the same hole or groove to move the annular ring in the circumferential or axial direction. In the device, two levers are provided, one lever is rotatably fitted to the stationary blade shaft at one end, and the other end is engaged with the groove or pin of the ring, and the pin, groove or hole is provided at the intermediate position. , The other lever is fixed to the vane shaft, and the other end is provided with a hole, a groove or a pin that engages with the pin, groove or hole at the intermediate position of the lever described above. apparatus.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP7884192U JPH0637597U (en) | 1992-10-21 | 1992-10-21 | Stationary blade angle changing device |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP7884192U JPH0637597U (en) | 1992-10-21 | 1992-10-21 | Stationary blade angle changing device |
Publications (1)
Publication Number | Publication Date |
---|---|
JPH0637597U true JPH0637597U (en) | 1994-05-20 |
Family
ID=13673053
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP7884192U Withdrawn JPH0637597U (en) | 1992-10-21 | 1992-10-21 | Stationary blade angle changing device |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPH0637597U (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2012184714A (en) * | 2011-03-07 | 2012-09-27 | Hitachi Ltd | Axial-flow compressor and modification method therefor |
-
1992
- 1992-10-21 JP JP7884192U patent/JPH0637597U/en not_active Withdrawn
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2012184714A (en) * | 2011-03-07 | 2012-09-27 | Hitachi Ltd | Axial-flow compressor and modification method therefor |
US9903389B2 (en) | 2011-03-07 | 2018-02-27 | Mitsubishi Hitachi Power Systems, Ltd. | Axial-flow compressor and modification method |
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Legal Events
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A300 | Withdrawal of application because of no request for examination |
Free format text: JAPANESE INTERMEDIATE CODE: A300 Effective date: 19970306 |